Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations
Author : George L. Pratt
Publisher :
Page : 110 pages
File Size : 34,77 MB
Release : 1952
Category : Airplanes
ISBN :